Harmonizing code from independent airborne aircraft identification systems

ABSTRACT

An Automatic Dependent Surveillance-Broadcast (ADS-B) system, and method of harmonizing a transponder Squawk code and an ADS-B system, ensures that a Squawk code broadcast by the ADS-B system matches the transponder Squawk code. The transponder Squawk code is transmitted from a transponder positioned onboard an aircraft, and the transmitted transponder Squawk code is received by a device positioned onboard the aircraft in which the transponder is installed. The ADS-B system is updated with the received transmitter squawk code. The squawk code is transmitted using the ADS-B system.

CROSS REFERENCE TO RELATED APPLICATIONS

This application is a continuation application of U.S. patent application Ser. No. 13/892,641, filed on May 13, 2013, which claims priority from U.S. provisional patent application Ser. No. 61/647,068, filed on May 15, 2012, and U.S. provisional patent application Ser. No. 61/683,854, filed on Aug. 16, 2012, the disclosures of which are hereby incorporated herein by reference in their entirety.

BACKGROUND OF THE INVENTION

The present invention relates to aircraft communication systems and, more particularly, to aircraft communication systems that provide identifying information about an aircraft, such as, but not limited to, transponders and Automatic Dependent Surveillance-Broadcast (ADS-B) systems.

The United States Federal Aviation Administration (FAA) has current plans to require that all aircraft include an Automatic Dependent Surveillance-Broadcast (ADS-B) system onboard by 2020. ADS-B systems are systems in which an aircraft repetitively broadcasts information about itself to both the air traffic control (ATC) system and any other aircraft within the vicinity of the broadcasting aircraft. The broadcast information includes, among other items, the aircraft's three-dimensional position and velocity, as well as an air traffic control assigned transponder code, also known as a Squawk code. In some instances, an aircraft equipped with the ADS-B system may also have an air traffic control radar beacon system (ATCRBS), which is a mode A/C transponder, onboard the aircraft. As is known in the art, the mode A/C transponder responds to certain interrogations by broadcasting a Squawk code that is received by air traffic control. Confusion at air traffic control may result if the mode A/C transponder Squawk code does not match the Squawk code broadcast by the ADS-B system from the same aircraft. The terms Squawk code and mode A Squawk code are used interchangeably throughout this document, but are intended to refer to the same code.

SUMMARY OF THE INVENTION

According to its various embodiments, the present invention provides methods and systems for ensuring that the aircraft identifying information, such as the Squawk code, broadcast by a transponder, such as an ATCRBS transponder, matches the aircraft identifying information broadcast by the ADS-B system. In other words, the various embodiments provide methods and systems for ensuring that an aircraft will not inadvertently broadcast different or multiple identification information through its transponder and its ADS-B system.

An Automatic Dependent Surveillance-Broadcast (ADS-B) system, according to an aspect of the invention, includes a transponder decoder having an input receiving a mode A/C transponder transmission from a transponder positioned aboard the aircraft in which the ABS-B system is positioned, a decoder decoding the mode A/C transponder transmission, and an output outputting the decoded mode A/C transponder transmission. A message formatter of the ADS-B system generates a message based on data received from the transponder decoder output. The message includes data identifying the squawk code. The transponder decoder and message formatter verify the received mode A/C transponder transmission is a squawk code from the aircraft in which the ADS-B system is installed. A wireless transmitter in communication with the message formatter wirelessly broadcasts the message.

An Automatic Dependent Surveillance-Broadcast (ADS-B) system, according to an aspect of the invention, includes a transponder decoder having a directional coupler receiving a transponder transmission via at least one antenna from the transponder positioned aboard the aircraft in which the ABS-B system is positioned, a decoder decoding the transponder transmission, and an output outputting the decoded transponder transmission. A logic device of the ADS-B system generates a message based on data received from the transponder decoder output. The message includes data identifying the squawk code. The transponder transmission is received in response to transmitting an interrogation signal from the logic device via the at least one antenna. A wireless transmitter is in communication with the logic device. The wireless transmitter wirelessly broadcasts the message via the directional coupler and the at least one antenna.

An Automatic Dependent Surveillance-Broadcast (ADS-B) system, according to an aspect of the invention, includes a transponder decoder having an input receiving a mode A/C transponder transmission from a transponder positioned in the aircraft in which the ADS-B system is positioned. A decoder of the transponder decoder decodes the mode A/C transponder transmission, and an output of the transponder decoder outputs the decoded mode A/C transponder transmission. A first transmitter sends an interrogation signal to activate the transponder positioned aboard the aircraft to send the received mode A/C transponder transmission.

The transponder decoder may receive the squawk code wirelessly from the transponder. The transponder decoder may also receive altitude information broadcast from the transponder and forward the altitude information to the message formatter for comparing the altitude information broadcast from the transponder to altitude information received from another source of altitude information.

The message formatter may determine that a transponder transmission is a squawk code, such as by determining that the transponder transmission has a value that is not the same value as altitude information for the aircraft. The message formatter may take an alternative action if it cannot determine that the transponder transmission is a squawk code. The alternative action may be to provide an indication to the pilot. The alternative action may be to send an interrogation signal to activate the transponder to send a squawk code. The wireless transmitter may be used to send the interrogation signal to the transponder.

The transponder may verify that a received transponder transmission is a transponder transmission from the aircraft in which the ADS-B system is installed by analyzing a signal strength of the received transponder transmission. The received transponder transmission is determined to be from the aircraft in which the ADS-B system is installed when the signal strength of the received transponder is above a threshold.

The ADS-B device may send an interrogation signal to activate the transponder to send a squawk code. The wireless transmitter may be used to send the interrogation signal to the transponder. The interrogation signal may be transmitted at an attenuated level. The message formatter may determine that the transponder is not transmitting. The message formatter may distinguish between the transponder not transmitting because i) the transponder is not operational or ii) the transponder is not being interrogated.

A transponder suppression bus input may be coupled to a transponder suppression bus to receive a signal to help differentiate between data transmitted by the transponder onboard the aircraft and data transmitted by any transponders off-board the aircraft. The transponder decoder may also receive IDENT information broadcast from the transponder and forward the IDENT information to the message formatter for formatting into the message.

The wireless transmitter may be a component of a Universal Access Transceiver (UAT).

These and other objects, advantages and features of this invention will become apparent upon review of the following specification in conjunction with the drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1 is a block diagram of an ADS-B system, according to an embodiment of the invention;

FIG. 2 is a flowchart of a method of harmonizing a transponder Squawk code and an ADS-B system such that an interrogation broadcast by the ADS-B system makes the transponder squawk;

FIG. 3 is a more detailed flowchart of the method of harmonizing a transponder Squawk code and an ADS-B system such that a Squawk code broadcast by the ADS-B system matches the transponder squawk in FIG. 2;

FIG. 4 is the same view as FIG. 1 of an alternative embodiment thereof; and

FIG. 5 is the same view as FIG. 2 of an alternative embodiment thereof.

DESCRIPTION OF THE EMBODIMENTS

Referring now to the drawings and the illustrative embodiments depicted therein, an Automatic Dependent Surveillance-Broadcast (ADS-B) system 220 for an aircraft is useful with a mode A/mode C transponder 224 having a transponder antenna 238 (FIG. 1). System 220 includes an ADS-B device 228 having a UAT transmitter and a low power transceiver antenna 240 that can output a mode A interrogation message directly to transponder 224. As disclosed in commonly assigned U.S. Patent Application Publication No. 2012/001788 A1, the disclosure of which is hereby incorporated herein by reference, such interrogation may be used wherever the transmission from transponder 224 equals the altitude information from the aircraft or ADS-B system 220 is otherwise unable to unambiguously determine the Squawk code. Since transceiver antenna 240 sends a mode A interrogation message, it can conclude that the transmission from transponder 224 is a mode A Squawk code. Transceiver antenna 240 can be separate from the UAT transceiver 230 used to transmit to the ground or to other aircraft or can be a combined transceiver that is capable of wireless communication with transponder antenna 238. If a common transceiver antenna is used, it would transmit at a lower power level to interrogate transponder 224 than would be used as a UAT transceiver mode.

System 220 includes a suppression bus 242 that is used to indicate that an L-band system onboard the aircraft is transmitting. It is used by ADS-B device 228 as a trigger to receive transmissions from transponder 224 to ensure that ADS-B device 228 is not intercepting a transponder transmission from a different aircraft. System 220 may further include a pilot control panel 261 that includes ADS-B system control device 262 that allows the pilot to manually enter a Squawk code into ADS-B device 228. Pilot control panel 261 may further include indicator 261 a to advise the pilot that the input altitude reported by transponder 224 does not match that reported by ADS-B control device 228, as will be discussed in more detail below. Also, indicator 261 b may be included to inform the pilot that the selected code as reported by transponder 224 does not match that entered into the ADS-B Squawk code entry device.

System 220 performs a control technique 1 that is based upon the requirement that the UAT device 228 must output the same mode A code as transponder 224. Referring now to FIG. 2, control technique 1 begins at 1 a with the pilot powering on and entering the squawk code in ADS-B device 228, such as with squawk code entry device 262. Transceiver antenna 240 sends a mode A interrogation message to transponder 224 at 2. Therefore, system 220 can conclude that the transmission from transponder 224 is a mode A Squawk code. When this occurs, the transponder is either off or in the standby mode or is on. If it is on, ADS-B device 228 receives a transmission from transponder 224 at 3. If it is determined at 3 that a response has not been received, then a transponder fail indication is made at 4 on an annunciator (not shown) or other visual or aural indicator. The fail indication may instruct the pilot to check that the transponder 224 is turned on.

If it is determined at 3 that a response is received from transponder 228, it is determined at 5 whether suppression bus 242 is active indicating that an L-band transmitter on the aircraft is transmitting. If so, the response originated with this aircraft. If it is determined at 5 that suppression bus 242 is not active then the response is ignored at 7. If it is determined at 5 that the suppression bus is active, it is determined at 6 whether the transmission is from transponder 224 by examining the format of the response. If it is determined at 6 that the response has the proper format for a transmission from transponder 224 then the response is decoded at 8 as a Mode A response from transponder 224. Otherwise it is ignored at 7.

The decoded Mode A response is compared with the code entered by the pilot with Squawk code entry device 262 at 9 and the result is evaluated at 10. If it is determined at 10 that the Mode A response decoded from transponder 224 is not different from the ADS-B code entered by the pilot, then no action is taken. However, if it is determined at 10 that a different code is entered in the ADS-B device than that decoded from transponder 224, an indication is made to the pilot at 11 such as by illuminating code miscompare attenuator 261 b or by some other visual or aural indication.

FIG. 3 illustrates a control technique 265 for ensuring that ADS-B device 228 only transmits as a Squawk code message to the air traffic control system or other aircraft in the vicinity of a mode A Squawk code message from transponder 224 that is more detailed than that illustrated in FIG. 2. With the pilot entering a Squawk code message (263 a) in transponder 224 and transponder 224 operational (264), ADS-B device 228 is also powered on at 266. The same Squawk code message that was entered in the transponder at 263 a is entered in ADS-B device 228 by the pilot via entry device 262 (263 b). It is determined at 267 whether more than a predetermined amount of time has passed since the last transmission has been received from transponder 224. Since transponder 224 is operational and has recently transmitted a message in response to a ground radar or from a TCAS unit onboard another aircraft, it will be determined at 267 that this predetermined time has not passed. It is then determined at 268 whether suppression line 242 is active, which will occur at least when transponder 224 is transmitting. If so, the message received by transceiver 240 is examined at 269 to determine if it has the format of a message from transponder 224. If so, the message is decoded at 270. Once the message is decoded, it is compared at 271 with the altitude information obtained by ADS-B device 228, such as from an altimeter that supplies altitude data to both transponder 224 and ADS-B device 228.

If the message decoded from transponder 224 is determined at 271 to not be the same as the altitude information, it is determined that the message must be a mode A Squawk code message so it is compared at 272 to the value of the Squawk code entered into ADS-B device 228. If these two Squawk codes are the same, this value of the Squawk code is the one to be used by ADS-B device 228 for future transmissions until it is changed by the pilot by entering a different Squawk code in transponder 224 and/or ADS-B device 228. If it is determined at 272 that these two Squawk codes are not the same, annunciator 261 b is actuated to instruct the pilot at 278 that the code entered in ADS-B device 228 does not match the code entered in transponder 224. This should prompt the pilot to change one of the codes to match the other.

If it is determined at 267 that more than a predetermined period of time, such as several seconds, has passed since last receipt of a transmission from transponder 224, then transponder 224 is likely not being interrogated by a ground radar or a TCAS unit in another aircraft. If it is determined at 267 that this period has not yet passed, it is determined at 268 whether suppression line 242 is active. If so, it is determined at 269 whether the device that is transmitting is transmitting a message having a protocol of a message transmitted by transponder 224. If not, the message is ignored at 273. This sequence is repeated until it is determined at 267 that more than the predetermined amount of time has passed. It is then determined at 274 whether a longer predetermined period of time, such as tens of seconds, has lapsed.

If it is determined at 274 that a longer predetermined period of time has not lapsed, ADS-B device 228 interrogates transponder 224 by sending an attenuated signal at 275 to transponder 224 having a format of a mode A code interrogation. This is accomplished either by sending the interrogation signal with an antenna 240 dedicated to communication with transponder 224 or by a UAT antenna 230 that is used both to communicate with transponder 224, at an attenuated signal level, and to generate ADS-B UAT signals external to the aircraft. It is then determined at 276 whether a response is received. If so, then it is concluded at 277 that it is a mode A Squawk message and it is used to compare with the Squawk code set for ADS-B device at 272. In this manner, it is possible to determine that the Squawk code for ADS-B device 228 is set to the same Squawk code as transponder 224, even if the transponder is not being interrogated by a ground radar or a TCAS unit of another aircraft.

If it is determined at 267 and 274 that a response is not received within the extended predetermined period of time after interrogation of transponder 224, a message is then given to the pilot at 278, such as with annunciator 261 b or other visual or aural warning indicator, instructing the pilot that the code entered with Squawk code entry device 262 does not match that entered in transponder 224 or the transponder is not operating properly or is turned off.

If it is determined at 276 that a message has not been received from transponder 224 even after having attempted to interrogate the transponder at 275, it is then concluded that the transponder is likely not turned on or has failed. An indication is given to the pilot at 280, such as using another annunciator (not shown) that the code cannot be set using control technique 265. The pilot may be instructed to turn the transponder on or to manually enter a Squawk code in ADS-B device, such as with Squawk code entry device 262, or may be optionally instructed to attempt to manually interrogate transponder 224. In this manner, it may be possible to enter a Squawk code in the ADS-B device, even if transponder 224 is powered off or has failed.

If it is determined at 267 that the lower predetermined period of time has not passed since the last transmission of transponder 224, since the transponder is being interrogated by a ground radar or a TCAS unit on another aircraft, it is determined at 268 whether suppression bus 242 is active and at 269 whether the transmission is from transponder 224. If so, the transmission is decoded at 270 and compared at 271 with the altitude data received by ADS-B device 228. If transponder 224 is set to a Squawk code that is indistinguishable from the altitude data received by ADS-B device 228, it will be determined at 281 that the transmission from transponder 224 is indistinguishable from the altitude value. As a result, the transmission from transponder 224 is not used to compare with the Squawk code in ADS-B device 228. Instead, transponder 224 is interrogated at 275 with UAT transceiver 240 at an attenuated signal level, or by separate transceiver 230. A response should be received at 276 since the transponder is presumably turned on and is not failed. Because the response is from a mode A interrogation signal, it is decoded at 277 and compared with the Squawk code set for ADS-B device 228 at 272.

Control device 261 may further include an Altitude Miscompare annunciator 261 a. Both transponder 224 and ADS-B device 228 may receive altitude data from a common altitude sensor (not shown). Therefore, the altitude information received from transponder 224 should match that received directly from the altitude sensor. If it does not match, this could be an indication of a failure in operation of either transponder 224 or ADS-B device 228. Such failure, if detected by a comparison of data decoded from transponder 224 and that received from the altitude sensor, is used to illuminate Altitude Miscompare annunciator 261 a or other such pilot warning technique including aural as well as visual.

While illustrated for use in ensuring that a common mode A Squawk code is used in the ADS-B device as in the transponder, the same technique could be used for mode C code signals or other types of code.

In an alternative embodiment, a system 220′ is generally the same as system 220 except that it includes a pilot control panel 261′ that includes a code miscompare indicator 261 b′ and an altitude miscompare indicator 261 a′ that are the same as code miscompare indicator 261 b and altitude miscompare indicator 261 a, respectively (FIGS. 4 and 5). However, system 220′ includes a sync input 262′ that is operable by the pilot to cause the message formatter of ADS-B unit 228′ to copy the transponder Squawk code that has been captured form transponder 224′. Thus, if the pilot observes that code miscompare indicator 261′ is actuated, sync control 262′ can be actuated manually by the pilot to cause ADS-B unit 228′ to copy the code of transponder 224′. This should result in the transponder and ADS-B system transmitting the same code which should result in code miscompare indicator 261 b′ being extinguished.

An advantage of system 262′ is that a separate pilot Squawk code entry device is not required in order to enter the Squawk code of ADS-B system 228′. Instead, a single “push to sync” push button could be used. However, a pilot Squawk code entry device for the ADS-B system could be provided, if desired, to have the pilot enter the same code into both the transponder and ADS-B system as previously described. Upon power-up of system 220′, ADS-B system 228′ may adopt a default Squawk code, the last known Squawk code, or the like. This should result in a mismatch between the Squawk codes of transponder 224′ and ADS-B system 228′. However, once the pilot operates sync input 262′, the mismatch should disappear.

In operation, referring to FIG. 5, control technique 1′ starts at 1 a′ by ADS-B system 228′ being powered. This should result in a Squawk code of a default value, the last used Squawk code, or some other value to be assigned to the ADS-B system. Control technique 1′ then performs the same general steps 2 through 11 as with control technique 1. However, if an indication is made to the pilot at 11 that the ADS-B code does not match that of the transponder, the pilot is able to manually actuate sync control 262′ at 11 a in order to copy the transponder mode A response of transponder 224′ into ADS-B system 228′. Upon the next transmission of ADS-B system 228′, the Squawk code will match that of transponder 224′.

While the foregoing description describes several embodiments of the present invention, it will be understood by those skilled in the art that variations and modifications to these embodiments may be made without departing from the spirit and scope of the invention, as defined in the claims below. The present invention encompasses all combinations of various embodiments or aspects of the invention described herein. It is understood that any and all embodiments of the present invention may be taken in conjunction with any other embodiment to describe additional embodiments of the present invention. Furthermore, any elements of an embodiment may be combined with any and all other elements of any of the embodiments to describe additional embodiments. 

The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows:
 1. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft comprising: a transponder decoder comprising an input configured to receive a mode A/C transponder transmission, a decoder decoding the mode A/C transponder transmission, and an output outputting the decoded mode A/C transponder transmission, wherein the mode A/C transponder transmission comprises a squawk code; a message formatter configured to generate a message based on data received from the transponder decoder output, the message including data identifying the squawk code, wherein the transponder decoder and message formatter are configured to verify that the received mode A/C transponder transmission is a squawk code from the aircraft in which the ADS-B system is installed; and a wireless transmitter in communication with the message formatter, wherein the wireless transmitter wirelessly broadcasts the message.
 2. The ADS-B system of claim 1, wherein the transponder decoder receives the squawk code wirelessly from the transponder.
 3. The ADS-B system of claim 1, wherein the transponder decoder also receives altitude information broadcast from the transponder and forwards the altitude information to the message formatter for formatting into the message.
 4. The ADS-B system of claim 1, wherein the message formatter verifies that a transponder transmission is a squawk code by determining that the transponder transmission has a value that is not the same value as altitude information for the aircraft.
 5. The ADS-B system of claim 1, wherein the transponder decoder verifies that a received transponder transmission is a transponder transmission from the aircraft in which the ADS-B system is installed by analyzing a signal strength of the received transponder transmission, wherein the received transponder transmission is from the aircraft in which the ADS-B system is installed when the signal strength of the received transponder is above a threshold.
 6. The ADS-B system of claim 1, wherein the message formatter causes an alternative action if the message formatter cannot verify that the transponder transmission is a squawk code.
 7. The ADS-B system of claim 6, wherein the alternative action comprises at least one chosen from (i) providing an indication to a pilot and (ii) sending an interrogation signal to activate the transponder to send a transmission.
 8. The ADS-B system of claim 1, wherein the ADS-B system sends an interrogation signal to activate the transponder to send a squawk code.
 9. The ADS-B system of claim 8, wherein the wireless transmitter sends the interrogation signal to the transponder.
 10. The ADS-B system of claim 8, wherein the interrogation signal is transmitted at an attenuated level.
 11. The ADS-B system of claim 1, wherein the message formatter determines that the transponder is not transmitting.
 12. The ADS-B system of claim 11, wherein the message formatter distinguishes between the transponder not transmitting because the transponder is not operational and because the transponder is not being interrogated.
 13. The ADS-B system of claim 12, wherein the message formatter notifies the pilot.
 14. The ADS-B system of claim 1 further comprising a transponder suppression bus input to be coupled to a transponder suppression bus within the aircraft in which the ADS-B system is installed, wherein the transponder suppression bus input responses to a signal when data is transmitted by the transponder onboard the aircraft to distinguish from data transmitted by any transponders off-board the aircraft.
 15. The ADS-B system of claim 1, wherein the transponder decoder also receives IDENT information broadcast from the transponder and forwards the IDENT information to the message formatter to be formatted into the message.
 16. The ADS-B system of claim 1, wherein the wireless transmitter is a component of a Universal Access Transceiver (UAT).
 17. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft comprising: a transponder decoder comprising an input receiving a mode A/C transponder transmission from a transponder positioned in the aircraft in which the ADS-B system is positioned, a decoder decoding the mode A/C transponder transmission, and an output outputting the decoded mode A/C transponder transmission, a first transmitter sending an interrogation signal to activate the transponder positioned aboard the aircraft to send the received mode A/C transponder transmissions; and a second transmitter coupled to the transponder decoder output and configured to wirelessly broadcast the decoded mode A/C transponder transmission data; wherein the second transmitter and the first transmitter are a combined transmitter that transmits at a lower power level when transmitting the interrogation signal than when transmitting the mode A/C transponder transmission.
 18. The ADS-B system of claim 17, wherein the transponder decoder input comprises an antenna to wirelessly detect the mode A/C transponder transmission.
 19. The ADS-B system of claim 17, wherein the decoded mode A/C transponder transmission is wirelessly broadcast using a Universal Access Transceiver (UAT).
 20. The ADS-B system of claim 17 further comprising a message formatter to verify that a received transponder transmission is a squawk code.
 21. The ADS-B system of claim 20, wherein the message formatter verifies that a received transponder transmission is a squawk code by determining that the received transponder transmission does not have a same value as pressure altitude information for the aircraft.
 22. The ADS-B system of claim 20, wherein the first transmitter sends the interrogation signal to activate the transponder if the message formatter cannot verify that the received transponder transmission is a squawk code.
 23. The ADS-B system of claim 20, wherein the message formatter determines that the transponder is not transmitting.
 24. The ADS-B system of claim 23, wherein the message formatter distinguishes between the transponder not transmitting because the transponder is not operational and not transmitting, and because the transponder is not being interrogated.
 25. The ADS-B system of claim 24, wherein the message formatter notifies the pilot.
 26. The ADS-B system of claim 18, wherein the antenna sends the interrogation signal to the transponder.
 27. An Automatic Dependent Surveillance-Broadcast (ADS-B) system for positioning in an aircraft having a transponder comprising: a transponder decoder comprising a directional coupler receiving a transponder transmission via at least one antenna, a decoder decoding the transponder transmission, and an output outputting the decoded transponder transmission, wherein the transponder transmission comprises a squawk code; a logic device generating a message based on data received from the transponder decoder output, the message including data identifying the squawk code, wherein the transponder transmission is received in response to transmitting an interrogation signal from the logic device via the at least one antenna, wherein the transponder decoder and the logic device are configured to verify the received transponder transmission is a squawk code from the aircraft in which the ADS-B is installed; and a wireless transmitter in communication with the logic device, wherein the wireless transmitter wirelessly broadcasts the message via the directional coupler and the at least one antenna.
 28. The ADS-B system of claim 27, wherein the at least one antenna comprises a first antenna for receiving the transponder transmission and for transmitting the message; and a second antenna for transmitting the interrogation signal.
 29. The ADS-B system of claim 27, wherein the at least one antenna is a single antenna.
 30. The ADS-B system of claim 29, wherein the directional coupler provides an attenuated path to the logic device.
 31. The ADS-B system of claim 30, wherein the decoder receives the transponder transmission via the attenuated path of the directional coupler, and wherein the decoder comprises a detector eliminating a carrier signal of the transponder transmission to produce a digital pulse stream as the decoded transponder transmission.
 32. The ADS-B system of claim 27, wherein the directional coupler provides a low-loss path to the wireless transmitter, wherein the wireless transmitter transmissions take place at 978 MHz.
 33. The ADS-B system of claim 27, wherein the interrogation signal is transmitted at an attenuated level.
 34. The ADS-B system of claim 27, wherein the interrogation signal comprises 970 MHz and 1030 MHz modulated pulses.
 35. The ADS-B system of claim 27, wherein the message is wirelessly broadcast using a Universal Access Transceiver (UAT).
 36. The ADS-B system of claim 27, wherein the transponder transmission comprises 1090 MHz modulated pulses.
 37. A method of automatically harmonizing a transponder squawk code and an Automatic Dependent Surveillance-Broadcast (ADS-B) system such that a squawk code broadcast by the ADS-B system matches the transponder squawk code, the method comprising: transmitting the transponder squawk code from a transponder positioned onboard an aircraft in which the ADS-B system is installed; receiving, with the ADS-B system, transponder squawk codes that include the transmitted transponder squawk code transmitted by the transponder; verifying that the received transponder squawk code is a squawk code from the transponder positioned onboard the aircraft; updating the ADS-B system with the received transponder squawk code; and broadcasting, with the ADS-B system, the squawk code.
 38. The method of claim 37, wherein the receiving the transmitted transponder squawk code is performed wirelessly using an antenna of the ADS-B system.
 39. The method of claim 37 further comprising receiving a signal from a transponder suppression bus, wherein the transponder suppression bus input receives a signal when data is transmitted by the transponder onboard the aircraft to distinguish from data transmitted by any transponders off-board the aircraft.
 40. The method of claim 37 further comprising receiving altitude information broadcast from the transponder positioned onboard the aircraft.
 41. The method of claim 40 further comprising determining that a transponder transmission is a squawk code by determining that the transponder transmission has a value that is not the same value as the received altitude information for the aircraft.
 42. The method of claim 41 further comprising taking alternative action if it cannot be determined that the transponder transmission is a squawk code.
 43. The method of claim 42, wherein the alternative action is chosen from (i) providing an indication to a pilot and (ii) sending an interrogation signal to activate the transponder to send a transmission.
 44. The method of claim 41 further comprising determining that the transponder is not transmitting.
 45. The method of claim 44, wherein the determining that the transponder is not transmitting comprises distinguishing between the transponder not transmitting because the transponder is not operational and because the transponder is not being interrogated.
 46. The method of claim 37 further comprising sending an interrogation signal with an antenna of the ADS-B system to activate the transponder to send the squawk code. 